JP2003025110A - Surface coated cemented carbide cutting tool excellent in surface lubricity for cutting chip - Google Patents
Surface coated cemented carbide cutting tool excellent in surface lubricity for cutting chipInfo
- Publication number
- JP2003025110A JP2003025110A JP2001211733A JP2001211733A JP2003025110A JP 2003025110 A JP2003025110 A JP 2003025110A JP 2001211733 A JP2001211733 A JP 2001211733A JP 2001211733 A JP2001211733 A JP 2001211733A JP 2003025110 A JP2003025110 A JP 2003025110A
- Authority
- JP
- Japan
- Prior art keywords
- layer
- cutting
- coating layer
- cemented carbide
- coated
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000005520 cutting process Methods 0.000 title claims abstract description 95
- 239000010936 titanium Substances 0.000 claims abstract description 64
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 47
- 239000000203 mixture Substances 0.000 claims abstract description 38
- 239000011195 cermet Substances 0.000 claims abstract description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 3
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 claims abstract description 3
- 239000010410 layer Substances 0.000 claims description 104
- 239000011247 coating layer Substances 0.000 claims description 50
- 230000001050 lubricating effect Effects 0.000 claims description 16
- 239000002131 composite material Substances 0.000 claims description 9
- 238000005240 physical vapour deposition Methods 0.000 claims description 7
- 229910052720 vanadium Inorganic materials 0.000 claims description 4
- 229910052758 niobium Inorganic materials 0.000 claims description 3
- 229910052715 tantalum Inorganic materials 0.000 claims description 3
- BVKZGUZCCUSVTD-UHFFFAOYSA-L Carbonate Chemical compound [O-]C([O-])=O BVKZGUZCCUSVTD-UHFFFAOYSA-L 0.000 claims description 2
- 150000004767 nitrides Chemical class 0.000 claims 1
- 238000005461 lubrication Methods 0.000 abstract description 5
- 229910045601 alloy Inorganic materials 0.000 abstract description 4
- 239000000956 alloy Substances 0.000 abstract description 4
- -1 compound nitride Chemical class 0.000 abstract description 2
- 150000001875 compounds Chemical class 0.000 abstract 4
- 239000000843 powder Substances 0.000 description 33
- 239000000463 material Substances 0.000 description 28
- 239000000758 substrate Substances 0.000 description 21
- 239000010935 stainless steel Substances 0.000 description 19
- 229910001220 stainless steel Inorganic materials 0.000 description 19
- 238000012360 testing method Methods 0.000 description 18
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 14
- 239000007789 gas Substances 0.000 description 10
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 8
- 238000007733 ion plating Methods 0.000 description 8
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 8
- 238000000034 method Methods 0.000 description 6
- 239000002994 raw material Substances 0.000 description 6
- 238000005553 drilling Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 238000001704 evaporation Methods 0.000 description 5
- 238000005259 measurement Methods 0.000 description 5
- 238000012545 processing Methods 0.000 description 5
- 102200029231 rs11551768 Human genes 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 4
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 4
- 239000012298 atmosphere Substances 0.000 description 4
- 230000007423 decrease Effects 0.000 description 4
- 230000008020 evaporation Effects 0.000 description 4
- 239000006104 solid solution Substances 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 229910001018 Cast iron Inorganic materials 0.000 description 3
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 3
- 229910001882 dioxygen Inorganic materials 0.000 description 3
- 238000010891 electric arc Methods 0.000 description 3
- 238000002156 mixing Methods 0.000 description 3
- 238000005245 sintering Methods 0.000 description 3
- 239000002345 surface coating layer Substances 0.000 description 3
- 238000003466 welding Methods 0.000 description 3
- 229910004349 Ti-Al Inorganic materials 0.000 description 2
- 229910004692 Ti—Al Inorganic materials 0.000 description 2
- 239000010730 cutting oil Substances 0.000 description 2
- 229910001873 dinitrogen Inorganic materials 0.000 description 2
- 238000000227 grinding Methods 0.000 description 2
- 230000020169 heat generation Effects 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 239000012495 reaction gas Substances 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 238000011160 research Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000007740 vapor deposition Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 229910001385 heavy metal Inorganic materials 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000012299 nitrogen atmosphere Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
Landscapes
- Drilling Tools (AREA)
- Cutting Tools, Boring Holders, And Turrets (AREA)
- Physical Vapour Deposition (AREA)
Abstract
Description
【発明の詳細な説明】
【0001】
【発明の属する技術分野】この発明は、切粉に対する表
面潤滑性にすぐれ、したがって特にステンレス鋼や軟鋼
などのきわめて粘性が高く、かつ切粉が切刃表面に溶着
し易い難削材の高速切削加工を、特に高切込みや高送り
などの重切削条件で用いた場合に、切刃に欠けやチッピ
ング(微小欠け)などの発生なく、すぐれた切削性能を
長期に亘って発揮する表面被覆超硬合金製切削工具(以
下、被覆超硬工具という)に関するものである。
【0002】
【従来の技術】一般に、被覆超硬工具には、各種の鋼や
鋳鉄などの被削材の旋削加工や平削り加工にバイトの先
端部に着脱自在に取り付けて用いられるスローアウエイ
チップ、前記被削材の穴あけ切削加工などに用いられる
ドリルやミニチュアドリル、さらに前記被削材の面削加
工や溝加工、肩加工などに用いられるソリッドタイプの
エンドミルなどがあり、また前記スローアウエイチップ
を着脱自在に取り付けて前記ソリッドタイプのエンドミ
ルと同様に切削加工を行うスローアウエイエンドミル工
具などが知られている。
【0003】また、上記の被覆超硬工具が、一般に、例
えば図1に概略説明図で示される物理蒸着装置の1種で
あるアークイオンプレーティング装置を用い、ヒータで
装置内を、例えば雰囲気を1.3×10-3Paの真空と
して、500℃の温度に加熱した状態で、アノード電極
と、所定組成を有するTi−Al合金がセットされたカ
ソード電極(蒸発源)との間にアーク放電を発生させ、
同時に装置内に反応ガスとしてメタンガスおよび/また
は窒素ガスを導入し、一方炭化タングステン(以下、W
Cで示す)基超硬合金または炭窒化チタン(以下、Ti
CNで示す)基サーメットからなり、かつ前記アノード
電極およびカソード電極と所定間隔をもって対向配置さ
れた工具基体(以下、これらを総称して超硬基体と云
う)には、例えば−120Vのバイアス電圧を印加した
条件で、前記超硬基体の表面に、例えば特開昭62−5
6565号公報に記載されるように、組成式:(Ti
1-XAlX)Nおよび同(Ti1-XAlX)C1-YNYで表わ
した場合、厚さ方向断面中央部を走査型電子顕微鏡で測
定して、原子比で、X:0.1〜0.7、Y:0.5〜
0.99、を満足するTiとAlの複合窒化物[以下、
(Ti,Al)Nで示す]層および複合炭窒化物[以
下、(Ti,Al)CNで示す]層のうちのいずれか、
または両方からなる硬質被覆層を0.5〜15μmの平
均層厚で物理蒸着することにより製造されることも知ら
れている。
【0004】
【発明が解決しようとする課題】近年の切削加工装置の
FA化はめざましく、一方で切削加工に対する省力化お
よび省エネ化、さらに低コスト化の要求は強く、これに
伴い、切削工具には1種類の工具でできるだけ多くの材
種の被削材を切削加工できる汎用性が求められると共
に、切削加工も高速化の傾向にあるが、上記の従来被覆
超硬工具においては、これを鋼や鋳鉄などの通常の条件
での切削加工に用いた場合には問題はないが、これをき
わめて粘性の高いステンレス鋼や軟鋼などの被削材の高
速切削に用いた場合には、これら被削材の切粉は、硬質
被覆層を構成する(Ti,Al)N層や(Ti,Al)
CN層に対する親和性が高いために、切刃表面に溶着し
易く、この溶着現象が原因で切刃に欠けやチッピングが
発生し、この結果比較的短時間で使用寿命に至るのが現
状である
【0005】
【課題を解決するための手段】そこで、本発明者等は、
上述のような観点から、特にステンレス鋼や軟鋼などの
切削加工に用いた場合にも、切刃表面に切粉の溶着し難
い被覆超硬工具を開発すべく研究を行った結果、(a)
上記の従来被覆超硬工具の表面に、表面被覆層として、
組成式:(Zr1- mMm)On (ただし、MはTi、V、
Nb、およびTaのうちの1種または2種以上を示
す)、で表わした場合、厚さ方向断面中央部をオージェ
分光分析装置で測定して、
m:0.01〜0.1、
n:1.7〜2.3、
を満足するZrとMの複合酸化物[以下(Zr,M)O
で示す]層を、0.5〜15μmの平均層厚で物理蒸着
すると、この結果の(Zr,M)O層が上記の通常の硬
質被覆層の表面に表面被覆層として物理蒸着された被覆
超硬工具においては、前記表面被覆層を構成する(Z
r,M)O層の被削材、特にステンレス鋼や軟鋼などの
粘性の高い難削材に対する親和性がきわめて低く、この
結果切刃に切粉が溶着することがない、すなわち前記
(Zr,M)O層がすぐれた表面潤滑性を発揮すること
から、切刃に欠けやチッピングの発生がなくなり、長期
に亘ってすぐれた切削性能を発揮するようになること。
【0006】(b)上記の物理蒸着法により形成された
(Zr,M)O層は、被覆層を構成する硬質被覆層であ
る(Ti,Al)N層および(Ti,Al)CN層との
密着性が十分でないので、上記の従来被覆超硬切削工具
の表面に前記(Zr,M)O層を直接形成してなる被覆
超硬切削工具においては、特に工具切刃に高い負荷のか
かるステンレス鋼や軟鋼などの高速切削を高切込みや高
送りなどの重切削条件で行った場合に前記(Zr,M)
O層に剥離が発生し易いこと。
【0007】(c)上記の従来被覆超硬切削工具を構成
する(Ti,Al)N層および(Ti,Al)CN層か
らなる硬質被覆層の表面に、まず、組成式:(Ti1-a
Ala)C1-bObおよび同(Ti1-aAla)C1-(b+c)O
bNcで表わした場合、厚さ方向断面中央部を走査型電子
顕微鏡で測定して、
a:0.1〜0.7、
b:0.1〜0.8、
c:0.05〜0.65
を満足するTiとAlの複合炭酸化物[以下、(Ti,
Al)COで示す]層および/またはTiとAlの複合
炭窒酸化物[以下、(Ti,Al)CNOで示す]層を
物理蒸着し、この上に上記(Zr,M)O層を物理蒸着
させると、この結果の(Zr,M)O層は上記(Ti,
Al)CO層および(Ti,Al)CNO層に著しく強
固に密着し、かつ前記(Ti,Al)CO層および(T
i,Al)CNO層は前記(Ti,Al)N層および
(Ti,Al)CN層からなる硬質被覆層に対する密着
性にもすぐれたものであるから、超硬基体に物理蒸着さ
れた前記硬質被覆層に、さらに前記(Ti,Al)CO
層および(Ti,Al)CNO層を介して前記(Zr,
M)O層を物理蒸着してなる被覆超硬切削工具は、ステ
ンレス鋼や軟鋼などの高速切削を、特に工具切刃に高い
負荷のかかる高切込みや高送りなどの重切削条件で行っ
ても前記(Zr,M)O層に剥離の発生なく、長期に亘
ってすぐれた耐摩耗性を発揮するようになること。以上
(a)〜(c)に示される研究結果を得たのである。
【0008】この発明は、上記の研究結果にもとづいて
なされたものであって、超硬基体の表面に、
(a)組成式:(Ti1-XAlX)Nおよび同(Ti1-X
AlX)C1-YNYで表わした場合、厚さ方向断面中央部
をオージェ分光分析装置で測定して、以下いずれも原子
比で、
X:0.1〜0.7、
Y:0.5〜0.99、
を満足する(Ti,Al)N層および(Ti,Al)C
N層のうちのいずれか、または両方からなり、かつ0.
5〜15μmの平均層厚を有する硬質被覆層、(b)組
成式:(Ti1-aAla)C1-bObおよび同(Ti1-aA
la)C1-(b+c)ObNcで表わした場合、厚さ方向断面中
央部をオージェ分光分析装置で測定して、
a:0.1〜0.7、
b:0.1〜0.8、
c:0.05〜0.65、
を満足する(Ti,Al)CO層および(Ti,Al)
CNO層のうちのいずれか、または両方からなり、かつ
0.1〜10μmの平均層厚を有する中間密着被覆層、
(c)組成式:(Zr1-mMm)On (ただし、MはT
i、V、Nb、およびTaのうちの1種または2種以上
を示す)で表わした場合、厚さ方向断面中央部をオージ
ェ分光分析装置で測定して、
m:0.01〜0.1、
n:ZrとMの合量に対する割合で1.7〜2.3、
を満足する(Zr,M)O層からなり、かつ0.5〜1
5μmの平均層厚を有する表面潤滑被覆層、以上(a)
〜(c)からなる被覆層を物理蒸着してなる、切粉に対
する表面潤滑性にすぐれた被覆超硬工具に特徴を有する
ものである。
【0009】つぎに、この発明の被覆超硬工具を構成す
る硬質被覆層、中間密着被覆層、および表面潤滑被覆層
について、上記の通りに数値限定した理由を説明する。
(a)硬質被覆層
硬質被覆層を構成する(Ti,Al)N層におけるAl
は高靭性を有するTiNに対してすぐれた高温硬さおよ
び耐熱性を付与し、もって一段の高温耐摩耗性向上を図
るために固溶するものであり、したがって組成式:(T
i1-XAlX)Nおよび同(Ti1-XAlX)C1-YNYのX
値が0.1未満では所望の高温耐摩耗性向上効果を確保
することができず、一方その値が0.7を越えると、切
刃に欠けやチッピングが発生し易くなると云う理由によ
りX値を0.1〜0.7(原子比)と定めたものであ
り、また、(Ti,Al)CN層におけるC成分には、
硬さを向上させる作用があるので、(Ti,Al)CN
層は上記(Ti,Al)N層に比して相対的に高い硬さ
をもつが、この場合C成分の割合が0.01未満、すな
わちY値が0.99を越えると所定の硬さ向上効果が得
られず、一方C成分の割合が0.5を越える、すなわち
Y値が0.5未満になると靭性が急激に低下するように
なることから、Y値を0.5〜0.99、望ましくは
0.55〜0.9と定めたのである。また、その平均層
厚が0.5μm未満では所望のすぐれた高温耐摩耗性を
確保することができず、一方その層厚が15μmを越え
ると、上記の潤滑被覆層の層厚と相俟って、切刃に欠け
やチッピング(微小欠け)が発生し易くなることから、
その平均層厚を0.5〜15μmと定めた。
【0010】(c)中間密着被覆層
同じく(Ti,Al)CO層および(Ti,Al)CN
O層におけるAlは高温硬さおよび耐熱性を向上させ、
もって一段の高温耐摩耗性向上を図るために固溶するほ
か、共通成分であるAlを含有する硬質被覆層との密着
性を向上させる作用を持つものであり、したがって組成
式:(Ti1-aAla)C1-bObおよび同(Ti1-aA
la)C1-(b+c)ObNcのa値が0.1未満では前記作用
に所望の向上効果が得られず、一方その値が0.7を越
えると、切刃に欠けやチッピングが発生し易くなると云
う理由によりa値を0.1〜0.7と定めたものであ
る。また、(Ti,Al)CO層および(Ti,Al)
CNO層におけるO成分には、表面潤滑被覆層との密着
性を向上させる作用があるが、上記組成式におけるb値
が0.1未満では所望の密着性向上効果が得られず、一
方その値が0.8を越えると、層自体の強度が急激に低
下し、これが欠けやチッピング発生の原因となると云う
理由によりb値を0.1〜0.8と定めた。さらに、上
記の(Ti,Al)CNO層は上記(Ti,Al)CO
層に比してN成分の含有によって相対的に高い靭性をも
つが、この場合N成分の割合(c値)が0.05未満で
は所定の靭性向上効果が得られず、一方N成分の割合
(c値)が0.65を越えると層自体の硬さが急激に低
下するようになることから、c値を0.05〜0.65
と定めたのである。また、その平均層厚が0.1μm未
満では、上記の硬質被覆層と表面潤滑被覆層との間に強
固な密着性を確保することができず、一方その平均層厚
が10μmを越えると、被覆層全体の脆化を促進し、切
刃に欠けやチッピングが発生し易くなることから、その
平均層厚を0.1〜10μmと定めた。
【0011】(c)表面潤滑被覆層
表面潤滑被覆層を構成する(Zr,M)O層は、Zr酸
化物に上記の通りの割合のM成分が固溶したものからな
る。前記Zr酸化物は、被削材、特にステンレス鋼や軟
鋼などの粘性の高い難削材に対する親和性がきわめて低
く、これは高い発熱を伴う高速切削加工でも変わらず、
したがって前記Zr酸化物層を物理蒸着してなる被覆超
硬工具はすぐれた表面潤滑性を発揮するようになること
から、切刃に切粉が溶着することがなくなり、この結果
切刃に欠けやチッピングの発生がなくなり、長期に亘っ
てすぐれた切削性能を発揮するようになるが、一方で前
記Zr酸化物層は脆く、強靭性に欠けるものであるた
め、摩耗進行が速いという問題点がある。しかし、前記
Zr酸化物層に、原子比で0.01〜0.1の割合でM
成分、すなわちTi、V、Nb、およびTaのうちの1
種または2種以上を固溶含有させると、この結果の(Z
r,M)O層はZr酸化物層と同等の著しくすぐれた表
面潤滑性を具備した上で、靭性および強度をもつように
なり、この結果耐摩耗性が著しく向上するようになる。
したがって、MのZrとの合量に占める割合(原子
比)、すなわちm値が0.01未満では所望の靭性およ
び強度を確保することができず、一方m値が0.1を超
えるとすぐれた表面潤滑性に低下傾向が現れるようにな
ることから、m値を0.01〜0.1と定めた。また、
同(Zr,M)O層における酸素(O)の原子比(n
値)を1.7〜2.3としたのは、その値が1.7未満
では所望のすぐれた表面潤滑性を確保することができ
ず、一方その値が2.3を越えると、層中に気孔が形成
され易くなり、健全な表面潤滑被覆層の安定的形成が難
しくなるという理由によるものである。さらに、同(Z
r,M)O層の平均層厚を、0.5〜15μmとしたの
は、その平均層厚が0.5μm未満では、所望の表面潤
滑性を確保することができず、一方この表面潤滑性付与
作用は15μmの平均層厚で十分満足に行うことができ
るという理由にもとづくものである。なお、上記の表面
潤滑被覆層の上に、必要に応じてTiN層を0.1〜2
μmの平均層厚で形成してもよく、これはTiN層が黄
金色の色調を有し、この色調によって切削工具の使用前
と使用後の識別が容易になるという理由からで、この場
合その平均層厚が0.1μm未満では前記色調の付与が
不十分であり、一方前記色調の付与は2μmまでの平均
層厚で十分である。
【0012】
【発明の実施の形態】ついで、この発明の被覆超硬切削
工具を実施例により具体的に説明する。
(実施例1)原料粉末として、いずれも1〜3μmの平
均粒径を有するWC粉末、TiC粉末、ZrC粉末、V
C粉末、TaC粉末、NbC粉末、Cr3 C2 粉末、T
iN粉末、TaN粉末、およびCo粉末を用意し、これ
ら原料粉末を、表1に示される配合組成に配合し、ボー
ルミルで72時間湿式混合し、乾燥した後、100MP
a の圧力で圧粉体にプレス成形し、この圧粉体を6P
aの真空中、温度:1400℃に1時間保持の条件で焼
結し、焼結後、切刃部分にR:0.05のホーニング加
工を施してISO規格・CNMG120408のチップ
形状をもったWC基超硬合金製の超硬基体A1〜A10
を形成した。
【0013】また、原料粉末として、いずれも0.5〜
2μmの平均粒径を有するTiCN(重量比でTiC/
TiN=50/50)粉末、Mo2 C粉末、ZrC粉
末、NbC粉末、TaC粉末、WC粉末、Co粉末、お
よびNi粉末を用意し、これら原料粉末を、表2に示さ
れる配合組成に配合し、ボールミルで24時間湿式混合
し、乾燥した後、100MPaの圧力で圧粉体にプレス
成形し、この圧粉体を2kPaの窒素雰囲気中、温度:
1500℃に1時間保持の条件で焼結し、焼結後、切刃
部分にR:0.03のホーニング加工を施してISO規
格・CNMG120408のチップ形状をもったTiC
N系サーメット製の超硬基体B1〜B6を形成した。
【0014】ついで、これら超硬基体A1〜A10およ
びB1〜B6を、アセトン中で超音波洗浄し、乾燥した
状態で、それぞれ図1に例示される通常のアークイオン
プレーティング装置に装入し、一方カソード電極(蒸発
源)として、種々の成分組成をもったTi−Al合金を
装着し、装置内を排気して1.3×10-3Paの真空に
保持しながら、ヒーターで装置内を500℃に加熱した
後、Arガスを装置内に導入して2.5PaのAr雰囲
気とし、この状態で超硬基体に−800Vのバイアス電
圧を印加して超硬基体表面をArガスボンバート洗浄
し、引き続いて3×10-3Paの真空に保持しながら、
ヒーターで装置内を600〜700℃の範囲内の所定の
温度に加熱した状態で、前記カソード電極とアノード電
極との間にアーク放電を発生させ、装置内に反応ガスと
して、メタンガスおよび/または窒素ガスを導入して所
定圧力の反応雰囲気とすると共に、前記超硬基体に印加
するバイアス電圧を−150Vとし、もって前記超硬基
体A1〜A10およびB1〜B6のそれぞれの表面に、
表3、4に示される目標組成および目標層厚の硬質被覆
層を蒸着形成することにより、図2(a)に概略斜視図
で、同(b)に概略縦断面図で示される形状を有する従
来被覆超硬工具としての従来表面被覆超硬合金製スロー
アウエイチップ(以下、従来被覆超硬チップと云う)1
〜22をそれぞれ製造した。
【0015】ついで、これら従来被覆超硬チップ1〜2
2のそれぞれの表面に、同じく図1のアークイオンプレ
ーティング装置にて、カソード電極(蒸発源)として、
中間密着被覆層形成用の種々の成分組成をもったTi−
Al合金、および表面潤滑被覆層形成用の種々の成分組
成をもったZr−M合金を装着し、装置内を排気して
1.3×10-3Paの真空に保持しながら、ヒーターで
装置内を620〜720℃の範囲内の所定の温度に加熱
した状態で、超硬基体に印加するパルスバイアス電圧を
−350Vとし、ついで装置内に反応ガスとして酸素ガ
ス、酸素ガスとメタンガスの混合ガス、あるいは酸素ガ
スとメタンガスと窒素ガスの混合ガスを導入して所定圧
力の反応雰囲気とし、かつ前記カソード電極とアノード
電極との間にアーク放電を発生させ、もって表5〜7に
示される目標組成および目標層厚の中間密着被覆層およ
び表面潤滑被覆層を形成することにより同じく図2に示
される形状をもった本発明被覆超硬工具としての本発明
表面被覆超硬合金製スローアウエイチップ(以下、本発
明被覆超硬チップと云う)1〜22をそれぞれ製造し
た。
【0016】なお、この結果得られた各種の被覆超硬チ
ップについて、これを構成する各種被覆層の組成および
層厚を、オージェ分光分析装置および走査型電子顕微鏡
を用いて測定したところ、表3〜7の目標組成および目
標層厚と実質的に同じ組成および平均層厚(任意5ヶ所
測定の平均値)を示した。
【0017】ついで、この結果得られた各種の被覆超硬
チップのうち、本発明被覆超硬チップ1〜16および従
来被覆超硬チップ1〜16について、
被削材:JIS・SUS304の丸棒、
切削速度:320m/min.、
切り込み:25mm、
送り:0.25mm/rev.、
切削時間:10分、
の条件でのステンレス鋼の乾式高速連続高切込み旋削加
工試験、
被削材:JIS・SUS304の長さ方向等間隔4本縦
溝入り丸棒、
切削速度:200m/min.、
切り込み:1.3mm、
送り:0.5mm/rev.、
切削時間:3分、
の条件でのステンレス鋼の乾式高速断続高送り旋削加工
試験、さらに、
被削材:JIS・S15Cの長さ方向等間隔4本縦溝入
り丸棒、
切削速度:280m/min.、
切り込み:1.5mm、
送り:0.55mm/rev.、
切削時間:5分、
の条件での軟鋼の乾式高速断続高送り旋削加工試験を行
い、いずれの旋削加工試験でも切刃の逃げ面摩耗幅を測
定した。
【0018】また、本発明被覆超硬チップ17〜22お
よび従来被覆超硬チップ17〜22については、
被削材:JIS・SUS304の丸棒、
切削速度:400m/min.、
切り込み:3.0mm、
送り:0.3mm/rev.、
切削時間:10分、
の条件でのステンレス鋼の乾式高速連続高切込み旋削加
工試験、
被削材:JIS・SUS304の長さ方向等間隔4本縦
溝入り丸棒、
切削速度:240m/min.、
切り込み:1.8mm、
送り:0.55mm/rev.、
切削時間:3分、
の条件でのステンレス鋼の乾式高速断続高送り旋削加工
試験、さらに、
被削材:JIS・S15Cの長さ方向等間隔4本縦溝入
り丸棒、
切削速度:340m/min.、
切り込み:1.5mm、
送り:0.48mm/rev.、
切削時間:5分、
の条件での軟鋼の乾式高速断続高送り旋削加工試験を行
い、いずれの旋削加工試験でも切刃部の逃げ面摩耗幅を
測定した。この測定結果を表8に示した。
【0019】
【表1】
【0020】
【表2】
【0021】
【表3】【0022】
【表4】
【0023】
【表5】【0024】
【表6】
【0025】
【表7】【0026】
【表8】【0027】(実施例2)原料粉末として、平均粒径:
5.5μmを有する中粗粒WC粉末、同0.8μmの微
粒WC粉末、同1.3μmのTaC粉末、同1.2μm
のNbC粉末、同1.2μmのZrC粉末、同2.3μ
mのCr3C2粉末、同1.5μmのVC粉末、同1.0
μmの(Ti,W)C粉末、および同1.8μmのCo
粉末を用意し、これら原料粉末をそれぞれ表9に示され
る配合組成に配合し、さらにワックスを加えてアセトン
中で24時間ボールミル混合し、減圧乾燥した後、10
0MPaの圧力で所定形状の各種の圧粉体にプレス成形
し、これらの圧粉体を、6Paの真空雰囲気中、7℃/
分の昇温速度で1370〜1470℃の範囲内の所定の
温度に昇温し、この温度に1時間保持後、炉冷の条件で
焼結して、直径が8mm、13mm、および26mmの
3種の超硬基体形成用丸棒焼結体を形成し、さらに前記
の3種の丸棒焼結体から、研削加工にて、表7に示され
る組合せで、切刃部の直径×長さがそれぞれ6mm×1
3mm、10mm×22mm、および20mm×45m
mの寸法をもった4枚刃スクエア形状の超硬基体(エン
ドミル)a〜hをそれぞれ製造した。
【0028】ついで、これらの超硬基体(エンドミル)
a〜hの表面に、アセトン中で超音波洗浄し、乾燥した
状態で、同じく図1に例示される通常のアークイオンプ
レーティング装置に装入し、上記実施例1と同一の条件
で、表10に示される目標組成および目標層厚の硬質被
覆層を蒸着形成することにより、図3(a)に概略正面
図で、同(b)に切刃部の概略横断面図で示される形状
を有する従来被覆超硬工具としての従来表面被覆超硬合
金製エンドミル(以下、従来被覆超硬エンドミルと云
う)1〜8をそれぞれ製造した。
【0029】さらに、上記の従来被覆超硬エンドミル1
〜8の表面に、同じくアークイオンプレーティング装置
にて、上記実施例1と同一の条件で、表11,12に示
される目標組成および目標層厚の中間密着被覆層および
表面潤滑被覆層を蒸着形成することにより同じく図3に
示される形状をもった本発明被覆超硬工具としての本発
明表面被覆超硬合金製エンドミル(以下、本発明被覆超
硬エンドミルと云う)1〜8をそれぞれ製造した。
【0030】また、この結果得られた各種の被覆超硬エ
ンドミルについて、これを構成する各種被覆層の組成お
よび層厚を、オージェ分光分析装置および走査型電子顕
微鏡を用いて測定したところ、表9〜12の目標組成お
よび目標層厚と実質的に同じ組成および平均層厚(任意
5ヶ所測定の平均値との比較)を示した。
【0031】つぎに、上記本発明被覆超硬エンドミル1
〜8および従来被覆超硬エンドミル1〜8のうち、本発
明被覆超硬エンドミル1〜3および従来被覆超硬エンド
ミル1〜3については、
被削材:平面寸法:100mm×250mm、厚さ:5
0mmのJIS・SUS304の板材、
切削速度:70m/min.、
溝深さ(切込み):5mm、
テーブル送り:120mm/分、
の条件でのステンレス鋼の湿式高速高切込み溝加工試験
(水溶性切削油使用)、本発明被覆超硬エンドミル4〜
6および従来被覆超硬エンドミル4〜6については、
被削材:平面寸法:100mm×250mm、厚さ:5
0mmのJIS・S15C板材、
切削速度:78m/min.、
溝深さ(切込み):8.2mm、
テーブル送り:128mm/分、
の条件での軟鋼の乾式高速高切込み溝加工試験、本発明
被覆超硬エンドミル7,8および従来被覆超硬エンドミ
ル7,8については、
被削材:平面寸法:100mm×250mm、厚さ:5
0mmのJIS・SUS304の板材、
切削速度:60m/min.、
溝深さ(切込み):9mm、
テーブル送り:95mm/分、
の条件でのステンレス鋼の湿式高速高送り溝加工試験
(水溶性切削油使用)、をそれぞれ行い、いずれの溝加
工試験でも外周刃の逃げ面摩耗量が使用寿命の目安とさ
れる0.1mmに至るまでの切削溝長を測定した。この
測定結果を表10、12にそれぞれ示した。
【0032】
【表9】
【0033】
【表10】
【0034】
【表11】
【0035】
【表12】
【0036】(実施例3)上記の実施例2で製造した直
径が8mm(超硬基体a〜c形成用)、13mm(超硬
基体d〜f形成用)、および26mm(超硬基体g、h
形成用)の3種の丸棒焼結体を用い、この3種の丸棒焼
結体から、研削加工にて、溝形成部の直径×長さがそれ
ぞれ4mm×13mm(超硬基体a’〜c’)、8mm
×22mm(超硬基体d’〜f’)、および16mm×
45mm(超硬基体g’、h’)の寸法をもった超硬基
体(ドリル)a’〜h’をそれぞれ製造した。
【0037】ついで、これらの超硬基体(ドリル)a’
〜h’の表面に、アセトン中で超音波洗浄し、乾燥した
状態で、同じく図1に例示される通常のアークイオンプ
レーティング装置に装入し、上記実施例1と同一の条件
で、表13に示される目標組成および目標層厚の硬質被
覆層を蒸着形成することにより、図4(a)に概略正面
図で、同(b)に溝形成部の概略横断面図で示される形
状を有する従来被覆超硬工具としての従来表面被覆超硬
合金製ドリル(以下、従来被覆超硬ドリルと云う)1〜
8をそれぞれ製造した。
【0038】さらに、上記の従来被覆超硬ドリル1〜8
の表面に、同じくアークイオンプレーティング装置に
て、上記実施例1と同一の条件で、表14、15に示さ
れる目標組成および目標層厚の中間密着被覆層および表
面潤滑被覆層を蒸着形成することにより、同じく図4に
示される形状をもった本発明被覆超硬工具としての本発
明表面被覆超硬合金製ドリル(以下、本発明被覆超硬ド
リルと云う)1〜8をそれぞれ製造した。
【0039】さらに、この結果得られた各種の被覆超硬
ドリルについて、これを構成する各種被覆層の組成およ
び層厚を、オージェ分光分析装置および走査型電子顕微
鏡を用いて測定したところ、表13〜15の目標組成お
よび目標層厚と実質的に同じ組成および平均層厚(任意
5ヶ所測定の平均値との比較)を示した。
【0040】つぎに、上記本発明被覆超硬ドリル1〜8
および従来被覆超硬ドリル1〜8のうち、本発明被覆超
硬ドリル1〜3および従来被覆超硬ドリル1〜3につい
ては、
被削材:平面寸法:100mm×250厚さ:50mm
のJIS・SUS304板材、
回転速度:4000min-1、
送り:0.25mm/rev、
の条件でのステンレス鋼の湿式高速高送り穴あけ加工試
験、本発明被覆超硬ドリル4〜6および従来被覆超硬ド
リル4〜6については、
被削材:平面寸法:100mm×250mm、厚さ:5
0mmのJIS・SUS304の板材、
回転速度:2200min-1、
送り:0.38mm/rev、
の条件でのステンレス鋼の湿式高速高送り穴あけ加工試
験、本発明被覆超硬ドリル7,8および従来被覆超硬ド
リル7,8については、
被削材:平面寸法:100mm×250mm、厚さ:5
0mmのJIS・S15Cの板材、
回転速度:2400min-1、
送り:0.55mm/rev、
の条件での軟鋼の湿式高速高送り穴あけ加工試験、をそ
れぞれ行い、いずれの湿式高速穴あけ加工試験(水溶性
切削油使用)でも先端切刃面の逃げ面摩耗幅が0.3m
mに至るまでの穴あけ加工数を測定した。この測定結果
を表13、15にそれぞれ示した。
【0041】
【表13】
【0042】
【表14】【0043】
【表15】
【0044】
【発明の効果】表3〜15に示される結果から、本発明
被覆超硬切削工具は、いずれも表面潤滑被覆層としての
(Zr,M)O層によって切刃表面にすぐれた潤滑性が
確保され、これが中間密着被覆層を構成する(Ti,A
l)CO層および(Ti,Al)CNO層と強固に密着
し、一方前記中間密着被覆層は上記の硬質被覆層を構成
する(Ti,Al)N層および(Ti,Al)CN層に
対しも強固に密着するようになるので、ステンレス鋼や
軟鋼の切削加工を高い発熱を伴う高速で、かつ高切込み
や高送りなどの重切削条件で行っても、高温に加熱され
た切粉が前記(Zr,M)O層に溶着することがなく、
切刃は常にすぐれた表面潤滑性を維持することから、切
刃への切粉溶着が原因のチッピングが切刃に発生するこ
とがなく、すぐれた耐摩耗性を発揮するのに対して、前
記(Zr,M)O層の形成のない従来被覆超硬工具にお
いては、切粉が硬質被覆層である(Ti,Al)N層お
よび(Ti,Al)CN層に溶着し易く、これが原因で
前記硬質被覆層が局部的に剥がし取られることから、切
刃にチッピングが発生し、比較的短時間で使用寿命に至
ることが明らかである。上述のように、この発明の被覆
超硬工具は、各種の鋼や鋳鉄などの通常の条件での切削
加工は勿論のこと、特に粘性が高く、切粉が切刃表面に
溶着し易いステンレス鋼や軟鋼などの高速切削加工を高
切込みや高送りなどの重切削条件で行っても切粉に対し
てすぐれた表面潤滑性を発揮し、汎用性のある切削性能
を示すものであるから、切削加工装置のFA化並びに切
削加工の省力化および省エネ化、さらに低コスト化に十
分満足に対応できるものである。Description: BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention has an excellent surface lubricating property against chips, and therefore, is particularly highly viscous, such as stainless steel or mild steel, and the chips have a cutting edge surface. Excellent cutting performance without chipping or chipping (small chipping) of the cutting edge when using high-speed cutting of difficult-to-cut materials that are easily welded to heavy metals, especially under heavy cutting conditions such as high cutting depth and high feed The present invention relates to a surface-coated cemented carbide cutting tool (hereinafter, referred to as a coated cemented carbide tool) that is exerted over a long period of time. 2. Description of the Related Art In general, a coated carbide tool is a throw-away tip which is removably attached to the tip of a cutting tool for turning or planing a work material such as steel or cast iron. Drills and miniature drills used for drilling and cutting of the work material, and solid type end mills used for face milling and grooving of the work material, shoulder processing, and the like. A throw-away end mill tool or the like which detachably attaches and performs cutting in the same manner as the solid type end mill is known. [0003] Further, the above-mentioned coated cemented carbide tool generally uses, for example, an arc ion plating apparatus which is a kind of a physical vapor deposition apparatus schematically shown in FIG. An arc discharge is caused between the anode electrode and a cathode electrode (evaporation source) on which a Ti-Al alloy having a predetermined composition is set while being heated to a temperature of 500 ° C. under a vacuum of 1.3 × 10 −3 Pa. Raises
At the same time, methane gas and / or nitrogen gas are introduced into the apparatus as a reaction gas, while tungsten carbide (hereinafter, W)
C) based cemented carbide or titanium carbonitride (hereinafter referred to as Ti
For example, a bias voltage of -120 V is applied to a tool base (hereinafter, referred to as a super hard base) made of a base cermet (indicated by CN) and opposed to the anode electrode and the cathode electrode at a predetermined interval. Under the conditions applied, the surface of the cemented carbide substrate is coated, for example, as disclosed in
No. 6,565, the composition formula: (Ti
1-X Al x ) N and (Ti 1-x Al x ) C 1-Y NY , the center of the cross section in the thickness direction was measured with a scanning electron microscope, and the atomic ratio was X: 0.1-0.7, Y: 0.5-
0.99 that satisfies 0.99.
One of a (Ti, Al) N] layer and a composite carbonitride [hereinafter, (Ti, Al) CN] layer;
Alternatively, it is also known to be manufactured by physical vapor deposition of a hard coating layer composed of both with an average layer thickness of 0.5 to 15 μm. [0004] In recent years, the use of FA in cutting equipment has been remarkable. On the other hand, there has been a strong demand for labor saving, energy saving, and further cost reduction for cutting work. In addition to the need for versatility to cut as many types of work materials as possible with a single type of tool, cutting tends to be faster, but in the above-mentioned conventional coated carbide tools, There is no problem when used for cutting under ordinary conditions such as steel or cast iron, but when used for high-speed cutting of work materials such as extremely viscous stainless steel and mild steel, The swarf of the material is composed of the (Ti, Al) N layer and the (Ti, Al)
Due to the high affinity for the CN layer, it is easily welded to the cutting blade surface, and this welding phenomenon causes chipping or chipping of the cutting blade, resulting in a relatively short service life. [0005] Accordingly, the present inventors have proposed:
From the above-mentioned viewpoints, a study was conducted to develop a coated carbide tool in which cutting chips are hardly welded to the surface of the cutting edge even when used for cutting of stainless steel, mild steel, and the like.
As a surface coating layer on the surface of the conventional coated carbide tool,
Composition formula: (Zr 1- m M m) O n ( however, M is Ti, V,
Nb, and one or more of Ta) are represented by the following formula: m: 0.01 to 0.1, n: 1.7 to 2.3, a composite oxide of Zr and M [hereinafter (Zr, M) O
The layer is physically vapor-deposited with an average layer thickness of 0.5 to 15 μm, and the resulting (Zr, M) O layer is physically vapor-deposited on the surface of the ordinary hard coating layer as a surface coating layer. In a cemented carbide tool, the surface coating layer is formed (Z
The (r, M) O layer has a very low affinity for a work material, particularly a high-viscosity hard-to-cut material such as stainless steel or mild steel, and as a result, no chips are welded to the cutting edge, that is, (Zr, M) Since the O layer exhibits excellent surface lubricity, chipping and chipping do not occur on the cutting edge, and excellent cutting performance is exhibited over a long period of time. (B) The (Zr, M) O layer formed by the above physical vapor deposition method is composed of a (Ti, Al) N layer and a (Ti, Al) CN layer which are hard coating layers constituting a coating layer. In the coated carbide cutting tool in which the (Zr, M) O layer is directly formed on the surface of the above-mentioned conventional coated carbide cutting tool, a high load is applied particularly to the tool cutting edge because the adhesiveness of the tool is not sufficient. When performing high-speed cutting of stainless steel or mild steel under heavy cutting conditions such as high depth of cut or high feed, the above (Zr, M)
The O layer is easily peeled. (C) First, on the surface of the hard coating layer composed of the (Ti, Al) N layer and the (Ti, Al) CN layer constituting the above-mentioned conventional coated carbide cutting tool, a composition formula: (Ti 1− a
Al a) C 1-b O b and the (Ti 1-a Al a) C 1- (b + c) O
When expressed in b N c, the cross section in the thickness direction central portion as measured with a scanning electron microscope, a: 0.1~0.7, b: 0.1~0.8 , c: 0.05~ A composite carbonate of Ti and Al satisfying 0.65 [hereinafter, (Ti,
Al) CO] layer and / or a composite carbonitride of Ti and Al [hereinafter referred to as (Ti, Al) CNO] layer is physically vapor-deposited, and the (Zr, M) O layer is Upon evaporation, the resulting (Zr, M) O layer would have the (Ti,
Al) CO layer and (Ti, Al) CNO layer are extremely firmly adhered, and the (Ti, Al) CO layer and (T
Since the (i, Al) CNO layer has excellent adhesion to the hard coating layer composed of the (Ti, Al) N layer and the (Ti, Al) CN layer, In the coating layer, the (Ti, Al) CO
Through the layer and the (Ti, Al) CNO layer.
M) A coated carbide cutting tool formed by physical vapor deposition of an O layer can perform high-speed cutting of stainless steel, mild steel, and the like, even under heavy cutting conditions such as high cutting and high feed, in which a high load is applied to the tool cutting edge. The (Zr, M) O layer exhibits excellent abrasion resistance over a long period of time without peeling. The research results shown in (a) to (c) above were obtained. The present invention has been made based on the results of the above-mentioned research, and comprises: (a) a composition formula: (Ti 1-X Al X ) N and (Ti 1-X)
Al x ) C 1-Y NY When measured in the thickness direction at the center of the cross section in the thickness direction using an Auger spectrometer, the following are all expressed by atomic ratios: X: 0.1 to 0.7, Y: 0 (Ti, Al) N layer and (Ti, Al) C
One or both of the N layers;
Hard layer having an average layer thickness of 5 to 15 [mu] m, (b) the composition formula: (Ti 1-a Al a ) C 1-b O b and the (Ti 1-a A
l a ) When represented by C 1-(b + c) O b N c , the center of the cross section in the thickness direction was measured by an Auger spectroscopic analyzer, and a: 0.1 to 0.7; (Ti, Al) CO layer and (Ti, Al) satisfying the following conditions: 1-0.8, c: 0.05-0.65
One of CNO layer, or consist of both, and an intermediate adhesion coating layer having an average layer thickness of 0.1 to 10 [mu] m, (c) the composition formula: (Zr 1-m M m ) O n ( however, M Is T
i, V, Nb, and Ta are represented by one or two or more), and the center of the cross section in the thickness direction is measured by an Auger spectrometer. m: 0.01 to 0.1 N: a (Zr, M) O layer satisfying 1.7 to 2.3 with respect to the total amount of Zr and M, and 0.5 to 1
A surface lubricating coating layer having an average layer thickness of 5 μm;
The present invention is characterized in that a coated carbide tool excellent in surface lubricity against chips is obtained by physical vapor deposition of a coating layer composed of (c). Next, the reason why the hard coating layer, the intermediate adhesion coating layer, and the surface lubrication coating layer constituting the coated carbide tool of the present invention are numerically limited as described above will be described. (A) Hard coating layer Al in the (Ti, Al) N layer constituting the hard coating layer
Is to impart excellent high-temperature hardness and heat resistance to TiN having high toughness and to form a solid solution in order to further improve high-temperature wear resistance. Therefore, the composition formula: (T
X of i 1-X Al X ) N and (Ti 1-X Al X ) C 1-Y NY
If the value is less than 0.1, the desired effect of improving the high-temperature wear resistance cannot be ensured. On the other hand, if the value exceeds 0.7, chipping and chipping are likely to occur on the cutting edge, so that the X value is increased. Is defined as 0.1 to 0.7 (atomic ratio), and the C component in the (Ti, Al) CN layer includes:
(Ti, Al) CN
The layer has a relatively high hardness as compared with the above (Ti, Al) N layer. In this case, when the ratio of the C component is less than 0.01, that is, when the Y value exceeds 0.99, the predetermined hardness is obtained. No improvement effect can be obtained, and on the other hand, when the ratio of the C component exceeds 0.5, that is, when the Y value is less than 0.5, the toughness rapidly decreases. 99, preferably 0.55 to 0.9. On the other hand, if the average layer thickness is less than 0.5 μm, the desired excellent high-temperature wear resistance cannot be ensured. On the other hand, if the average layer thickness exceeds 15 μm, the above-mentioned thickness of the lubricating coating layer may not be obtained. Since chipping and chipping (small chipping) easily occur in the cutting blade,
The average layer thickness was determined to be 0.5 to 15 μm. (C) Intermediate adhesion coating layer (Ti, Al) CO layer and (Ti, Al) CN
Al in the O layer improves high-temperature hardness and heat resistance,
Accordingly, it has a function of improving the adhesion to a hard coating layer containing Al as a common component in addition to forming a solid solution in order to further improve the high-temperature wear resistance. Therefore, the composition formula: (Ti 1− a Al a ) C 1-b O b and (Ti 1-a A
l a) C 1- (b + c) O b a value of N c is not obtained the desired improvement in the working is less than 0.1, whereas when the value exceeds 0.7, the cutting edge The value a is set to 0.1 to 0.7 for the reason that chipping or chipping is likely to occur. The (Ti, Al) CO layer and the (Ti, Al)
The O component in the CNO layer has an effect of improving the adhesion to the surface lubricating coating layer, but if the b value in the above composition formula is less than 0.1, the desired effect of improving the adhesion cannot be obtained. Exceeds 0.8, the b value is set to 0.1 to 0.8 for the reason that the strength of the layer itself sharply decreases, which causes chipping or chipping. Further, the (Ti, Al) CNO layer is formed of the (Ti, Al) CO
Although the toughness is relatively high due to the inclusion of the N component as compared to the layer, in this case, if the ratio (c value) of the N component is less than 0.05, a predetermined toughness improving effect cannot be obtained. When the (c value) exceeds 0.65, the hardness of the layer itself rapidly decreases, so the c value is set to 0.05 to 0.65.
It was decided. Further, if the average layer thickness is less than 0.1 μm, it is not possible to ensure strong adhesion between the hard coating layer and the surface lubricating coating layer, while if the average layer thickness exceeds 10 μm, Since the embrittlement of the entire coating layer is promoted, and chipping and chipping easily occur in the cutting edge, the average layer thickness is set to 0.1 to 10 μm. (C) Surface Lubricating Coating Layer The (Zr, M) O layer constituting the surface lubricating coating layer is made of a Zr oxide in which the above-mentioned ratio of the M component is dissolved in a solid solution. The Zr oxide has a very low affinity for work materials, particularly high-viscosity hard-to-cut materials such as stainless steel and mild steel, which is unchanged even in high-speed cutting with high heat generation.
Therefore, the coated carbide tool formed by physical vapor deposition of the Zr oxide layer exhibits excellent surface lubricity, so that chips are not welded to the cutting edge. Chipping does not occur, and excellent cutting performance is exhibited over a long period of time. However, since the Zr oxide layer is brittle and lacks toughness, there is a problem that wear progresses rapidly. . However, M is added to the Zr oxide layer at an atomic ratio of 0.01 to 0.1.
One of the components, Ti, V, Nb, and Ta
When one or more species are contained in a solid solution, (Z
The (r, M) O layer has remarkably excellent surface lubricity equivalent to that of the Zr oxide layer, and also has toughness and strength. As a result, wear resistance is significantly improved.
Therefore, if the ratio (atomic ratio) of M to the total amount with Zr, that is, the value of m is less than 0.01, desired toughness and strength cannot be ensured. On the other hand, if the value of m exceeds 0.1, it is excellent. Since the surface lubricity tends to decrease, the m value is set to 0.01 to 0.1. Also,
The atomic ratio (n) of oxygen (O) in the (Zr, M) O layer
The value of 1.7 to 2.3 means that if the value is less than 1.7, the desired excellent surface lubricating property cannot be ensured. On the other hand, if the value exceeds 2.3, the layer This is because pores are easily formed therein, and it is difficult to stably form a sound surface lubricating coating layer. Furthermore, the same (Z
The reason why the average layer thickness of the (r, M) O layer is 0.5 to 15 μm is that if the average layer thickness is less than 0.5 μm, desired surface lubricity cannot be ensured. The property-imparting action is based on the reason that an average layer thickness of 15 μm can be sufficiently performed. In addition, a TiN layer may be formed on the surface lubricating coating layer by 0.1 to 2 if necessary.
It may be formed with an average layer thickness of μm, since the TiN layer has a golden hue, which makes it easier to distinguish the cutting tool before and after use, in this case If the average layer thickness is less than 0.1 μm, the application of the color tone is insufficient, while the application of the color tone is sufficient if the average layer thickness is up to 2 μm. Next, the coated carbide cutting tool of the present invention will be specifically described with reference to examples. (Example 1) As raw material powders, WC powder, TiC powder, ZrC powder, V
C powder, TaC powder, NbC powder, Cr 3 C 2 powder, T
An iN powder, a TaN powder, and a Co powder were prepared, and these raw material powders were blended in the blending composition shown in Table 1, wet-mixed in a ball mill for 72 hours, dried, and then dried.
a into a green compact at the pressure of a
sintering in a vacuum at a temperature of 1400 ° C. for 1 hour, and after sintering, the cutting edge portion is subjected to a honing process of R: 0.05 to form a WC having a chip shape of ISO standard CNMG120408. Substrates A1 to A10 made of base cemented carbide
Was formed. In addition, as raw material powders,
TiCN having an average particle size of 2 μm (by weight ratio TiC /
(TiN = 50/50) powder, Mo 2 C powder, ZrC powder, NbC powder, TaC powder, WC powder, Co powder, and Ni powder were prepared, and these raw material powders were blended into the composition shown in Table 2. After wet-mixing with a ball mill for 24 hours and drying, the mixture is pressed into a green compact at a pressure of 100 MPa, and the green compact is heated in a nitrogen atmosphere of 2 kPa at a temperature of:
Sintered under the condition of holding at 1500 ° C. for 1 hour, and after sintering, the cutting edge portion is subjected to a honing process of R: 0.03 to obtain a TiC having a chip shape conforming to ISO standard, CNMG120408.
Carbide substrates B1 to B6 made of N-based cermet were formed. Next, these super-hard substrates A1 to A10 and B1 to B6 are ultrasonically cleaned in acetone, dried, and charged into a usual arc ion plating apparatus illustrated in FIG. 1, respectively. On the other hand, as a cathode electrode (evaporation source), Ti-Al alloys having various component compositions are mounted, and the inside of the apparatus is evacuated and kept at a vacuum of 1.3 × 10 −3 Pa while the inside of the apparatus is heated by a heater. After heating to 500 ° C., an Ar gas was introduced into the apparatus to form an Ar atmosphere of 2.5 Pa. In this state, a bias voltage of −800 V was applied to the super hard substrate to clean the surface of the super hard substrate by Ar gas bombardment. Then, while maintaining a vacuum of 3 × 10 −3 Pa,
An arc discharge is generated between the cathode electrode and the anode electrode while the inside of the apparatus is heated to a predetermined temperature within the range of 600 to 700 ° C. by a heater, and methane gas and / or nitrogen are used as reaction gases in the apparatus. A gas is introduced to form a reaction atmosphere at a predetermined pressure, and a bias voltage applied to the cemented carbide substrate is set to -150 V, so that each surface of the cemented carbide substrates A1 to A10 and B1 to B6 is
By forming a hard coating layer having a target composition and a target layer thickness shown in Tables 3 and 4 by vapor deposition, it has a shape shown in a schematic perspective view in FIG. 2A and a schematic longitudinal sectional view in FIG. Conventional surface coated cemented carbide throwaway inserts as conventional coated carbide tools (hereinafter referred to as conventional coated carbide tips) 1
~ 22 were each manufactured. Next, the conventional coated cemented carbide tips 1-2
2 on each surface as a cathode electrode (evaporation source) by the arc ion plating apparatus of FIG.
Ti- with various component compositions for forming an intermediate adhesion coating layer
An Al alloy and a Zr-M alloy having various component compositions for forming a surface lubricating coating layer are mounted, and while the inside of the apparatus is evacuated and maintained at a vacuum of 1.3 × 10 −3 Pa, the apparatus is heated by a heater. With the inside heated to a predetermined temperature within the range of 620 to 720 ° C., the pulse bias voltage applied to the carbide substrate is set to −350 V. Then, oxygen gas, a mixed gas of oxygen gas and methane gas is used as a reaction gas in the apparatus. Alternatively, a mixed gas of oxygen gas, methane gas, and nitrogen gas is introduced to form a reaction atmosphere at a predetermined pressure, and an arc discharge is generated between the cathode electrode and the anode electrode, thereby obtaining a target composition shown in Tables 5 to 7. By forming an intermediate adhesion coating layer and a surface lubricating coating layer having a target layer thickness, the surface-coated cemented carbide of the present invention as the coated carbide tool of the present invention also having the shape shown in FIG. Lore way chip (hereinafter, the present invention refers to the coating hard tip) 1 to 22 were prepared, respectively. The compositions and thicknesses of the various coating layers constituting the various coated carbide tips obtained as a result were measured using an Auger spectrometer and a scanning electron microscope. 7, the composition and the average layer thickness (average values measured at five arbitrary points) were substantially the same as the target composition and the target layer thickness. Next, among the various coated carbide tips obtained as a result, the coated carbide tips 1 to 16 of the present invention and the conventional coated carbide tips 1 to 16 were prepared. Cutting speed: 320 m / min. Infeed: 25 mm Feed: 0.25 mm / rev. , Cutting time: 10 minutes, Dry high-speed continuous high-depth turning test on stainless steel under the following conditions: Work material: JIS SUS304, 4 longitudinally-spaced round bars at equal intervals in the longitudinal direction, Cutting speed: 200 m / min . Infeed: 1.3 mm Feed: 0.5 mm / rev. , Cutting time: 3 minutes, Dry high-speed intermittent high-feed turning test of stainless steel under the following conditions: Work material: JIS S15C, lengthwise round bar with four longitudinal grooves, Cutting speed: 280 m / Min. Infeed: 1.5 mm Feed: 0.55 mm / rev. A dry high-speed intermittent high-feed turning test of mild steel was performed under the following conditions: cutting time: 5 minutes, and the flank wear width of the cutting edge was measured in each turning test. The coated super hard tips 17 to 22 of the present invention and the conventional super hard tips 17 to 22 are as follows: work material: round bar of JIS SUS304, cutting speed: 400 m / min. Infeed: 3.0 mm Feed: 0.3 mm / rev. , Cutting time: 10 minutes, Dry high-speed continuous high-incision turning test of stainless steel under the following conditions: Work material: JIS SUS304, 4 longitudinally spaced round bars with equal length, Cutting speed: 240 m / min . Infeed: 1.8 mm Feed: 0.55 mm / rev. , Cutting time: 3 minutes, Dry high-speed intermittent high-feed turning test of stainless steel under the following conditions: Work material: JIS S15C, 4 longitudinally-spaced round bars at regular intervals in the longitudinal direction, Cutting speed: 340 m / Min. Infeed: 1.5 mm Feed: 0.48 mm / rev. A dry high-speed intermittent high-feed turning test of mild steel was performed under the following conditions: cutting time: 5 minutes, and the flank wear width of the cutting edge was measured in each turning test. Table 8 shows the measurement results. [Table 1] [Table 2] [Table 3] [Table 4] [Table 5] [Table 6] [Table 7] [Table 8] (Example 2) As raw material powder, average particle size:
Medium coarse WC powder having 5.5 μm, fine WC powder of 0.8 μm, TaC powder of 1.3 μm, 1.2 μm
NbC powder, 1.2 μm ZrC powder, 2.3 μm
m Cr 3 C 2 powder, 1.5 μm VC powder, 1.0
μm of (Ti, W) C powder and 1.8 μm of Co
Powders were prepared, and each of these raw material powders was blended into the blending composition shown in Table 9, further added with wax, and ball-mixed in acetone for 24 hours, and dried under reduced pressure.
Press molding at a pressure of 0 MPa into various green compacts of a predetermined shape, and pressing these green compacts in a vacuum atmosphere of 6 Pa at 7 ° C. /
The temperature was raised to a predetermined temperature in the range of 1370 to 1470 ° C. at a heating rate of 1 minute, kept at this temperature for 1 hour, and then sintered under the condition of furnace cooling to obtain a sample having a diameter of 8 mm, 13 mm, and 26 mm. Kinds of round bar sintered bodies for forming a cemented carbide substrate are formed, and the above three kinds of round bar sintered bodies are subjected to grinding processing in a combination shown in Table 7 to obtain the diameter × length of the cutting edge portion. Is 6mm × 1 each
3mm, 10mm x 22mm, and 20mm x 45m
Carbide substrates (end mills) a to h each having a square shape and four blades having a size of m were manufactured. Next, these carbide substrates (end mills)
The surfaces a to h were ultrasonically cleaned in acetone, dried, and charged into a normal arc ion plating apparatus also illustrated in FIG. 1 under the same conditions as in Example 1 above. By vapor-depositing and forming a hard coating layer having a target composition and a target layer thickness shown in FIG. 10, the shape shown in the schematic front view in FIG. Conventional surface-coated cemented carbide end mills (hereinafter, referred to as conventional coated carbide end mills) 1 to 8 as conventional coated cemented carbide tools were manufactured. Further, the above-mentioned conventional coated carbide end mill 1
The intermediate adhesion coating layer and the surface lubricating coating layer having the target compositions and target layer thicknesses shown in Tables 11 and 12 were deposited on the surfaces of Nos. 1 to 8 by the same arc ion plating apparatus under the same conditions as in Example 1 above. By forming the same, end mills 1 to 8 made of the surface coated cemented carbide of the present invention (hereinafter referred to as coated carbide end mills of the present invention) as coated carbide tools of the present invention having the shape shown in FIG. . The compositions and thicknesses of the various coating layers constituting the various coated carbide end mills obtained as a result were measured using an Auger spectrometer and a scanning electron microscope. The composition and the average layer thickness (compared with the average value of measurement at five arbitrary positions) were substantially the same as the target compositions and the target layer thicknesses of No. to No. 12. Next, the coated carbide end mill 1 of the present invention will be described.
-8 and the conventional coated carbide end mills 1-8, the coated carbide end mills 1-3 of the present invention and the conventional coated carbide end mills 1-3 are: work material: plane dimension: 100 mm × 250 mm, thickness: 5
JIS SUS304 plate material of 0 mm, Cutting speed: 70 m / min. , Groove depth (cut): 5 mm, Table feed: 120 mm / min, Wet high-speed, high-cut groove processing test (using water-soluble cutting oil) for stainless steel under the conditions:
6 and the conventional coated carbide end mills 4 to 6 are: work material: plane dimension: 100 mm × 250 mm, thickness: 5
0 mm JIS S15C plate, Cutting speed: 78 m / min. , Groove depth (cut): 8.2 mm, table feed: 128 mm / min, dry high-speed, high-cut groove machining test of mild steel, coated carbide end mills 7, 8 according to the present invention and conventional coated carbide end mill 7, About 8, work material: plane dimension: 100 mm x 250 mm, thickness: 5
0 mm JIS SUS304 plate, Cutting speed: 60 m / min. , Groove depth (cut): 9 mm, Table feed: 95 mm / min, Wet stainless steel wet high-speed high-feed groove processing test (using water-soluble cutting oil). The cutting groove length was measured until the flank wear amount of the blade reached 0.1 mm, which is a standard for the service life. The measurement results are shown in Tables 10 and 12, respectively. [Table 9] [Table 10] [Table 11] [Table 12] (Example 3) The diameters of 8 mm (for forming the super-hard substrates a to c), 13 mm (for forming the super-hard substrates d to f), and 26 mm (for the super-hard substrate g) produced in Example 2 described above. h
(For forming), the diameter x length of the groove forming portion was 4 mm x 13 mm (the carbide substrate a ') by grinding from the three types of round rod sintered bodies. ~ C '), 8mm
× 22 mm (carbide substrate d ′ to f ′) and 16 mm ×
Carbide substrates (drills) a 'to h' each having a size of 45 mm (carbide substrates g 'and h') were manufactured. Next, these carbide substrates (drills) a '
Hh ′ was ultrasonically cleaned in acetone, dried and charged in a usual arc ion plating apparatus also illustrated in FIG. 1 under the same conditions as in Example 1 above. By evaporating and forming the hard coating layer having the target composition and target layer thickness shown in FIG. 13, the shape shown in the schematic front view in FIG. 4A and the schematic cross-sectional view of the groove forming part in FIG. Drills made of conventional surface-coated cemented carbide as conventional coated carbide tools (hereinafter referred to as conventional coated carbide drills)
8 were each produced. Further, the above-mentioned conventional coated carbide drills 1 to 8
The intermediate adhesion coating layer and the surface lubrication coating layer having the target compositions and the target layer thicknesses shown in Tables 14 and 15 are formed by vapor deposition on the surface of the substrate under the same conditions as in Example 1 by the same arc ion plating apparatus. Accordingly, drills made of the surface-coated cemented carbide of the present invention (hereinafter, referred to as coated carbide drills of the present invention) 1 to 8 as the coated carbide tools of the present invention also having the shape shown in FIG. 4 were manufactured. Further, with respect to the various coated carbide drills obtained as a result, the compositions and thicknesses of various coating layers constituting the drills were measured using an Auger spectrometer and a scanning electron microscope. The composition and the average layer thickness (compared to the average value of measurement at five arbitrary points) were substantially the same as the target composition and the target layer thickness of No. to No. 15. Next, the above-mentioned coated carbide drills 1-8 of the present invention are coated.
Of the coated carbide drills 1 to 8 of the present invention, the coated carbide drills 1 to 3 and the coated carbide drills 1 to 3 of the present invention are as follows: Work material: plane dimension: 100 mm × 250 thickness: 50 mm
JIS SUS304 plate material, rotational speed: 4000 min -1 , feed: 0.25 mm / rev, wet high-speed high-feed drilling test of stainless steel under the conditions, coated carbide drills of the present invention 4 to 6 and conventional coated carbide For drills 4 to 6, Work material: Plane dimensions: 100 mm x 250 mm, Thickness: 5
0 mm JIS SUS304 plate, rotating speed: 2200 min -1 , feed: 0.38 mm / rev, wet wet high-speed high-drilling test of stainless steel, coated carbide drills 7, 8 according to the present invention and conventional coated For carbide drills 7 and 8, Work material: Plane dimensions: 100 mm x 250 mm, thickness: 5
JIS S15C plate material of 0 mm, rotational speed: 2400 min -1 , feed: 0.55 mm / rev, and wet high-speed high-feed drilling test of mild steel were performed. Flank wear width of the tip cutting edge is 0.3m
The number of drilling operations up to m was measured. The measurement results are shown in Tables 13 and 15, respectively. [Table 13] [Table 14] [Table 15] From the results shown in Tables 3 to 15, all of the coated carbide cutting tools of the present invention have excellent lubrication on the cutting edge surface by the (Zr, M) O layer as the surface lubricating coating layer. , Which constitutes the intermediate adhesion coating layer (Ti, A
1) firmly adheres to the CO layer and the (Ti, Al) CNO layer, while the intermediate adhesion coating layer is in contact with the (Ti, Al) N layer and the (Ti, Al) CN layer constituting the hard coating layer. Since it comes to adhere firmly, even when cutting stainless steel and mild steel at high speed with high heat generation, and under heavy cutting conditions such as high cutting and high feed, the chips heated to high temperature are Without welding to the (Zr, M) O layer,
Since the cutting edge always maintains excellent surface lubricity, chipping due to chip welding to the cutting edge does not occur on the cutting edge, and the cutting edge exhibits excellent wear resistance. In the conventional coated cemented carbide tool having no (Zr, M) O layer, the chips tend to adhere to the hard coating layers (Ti, Al) N layer and (Ti, Al) CN layer. Since the hard coating layer is locally peeled off, it is clear that chipping occurs in the cutting blade and the service life is relatively short. As described above, the coated cemented carbide tool of the present invention can be used not only for cutting under various conditions such as steel and cast iron, but also for stainless steel, which is particularly highly viscous and easily adheres to the cutting blade surface. Even when high-speed cutting of steel or mild steel is performed under heavy cutting conditions such as high depth of cut and high feed, it exhibits excellent surface lubricity against chips and exhibits versatile cutting performance. It is possible to satisfactorily cope with the FA of the processing device, the labor saving and the energy saving of the cutting process, and the cost reduction.
【図面の簡単な説明】
【図1】アークイオンプレーティング装置の概略説明図
である。
【図2】(a)は被覆超硬チップの概略斜視図、(b)
は被覆超硬チップの概略縦断面図である。
【図3】(a)は被覆超硬エンドミル概略正面図、
(b)は同切刃部の概略横断面図である。
【図4】(a)は被覆超硬ドリルの概略正面図、(b)
は同溝形成部の概略横断面図である。BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a schematic explanatory view of an arc ion plating apparatus. FIG. 2A is a schematic perspective view of a coated carbide tip, and FIG.
1 is a schematic vertical sectional view of a coated carbide tip. FIG. 3 (a) is a schematic front view of a coated carbide end mill,
(B) is a schematic transverse sectional view of the cutting blade portion. FIG. 4A is a schematic front view of a coated carbide drill, and FIG.
FIG. 3 is a schematic cross-sectional view of the groove forming portion.
─────────────────────────────────────────────────────
【手続補正書】
【提出日】平成13年8月22日(2001.8.2
2)
【手続補正1】
【補正対象書類名】明細書
【補正対象項目名】0017
【補正方法】変更
【補正内容】
【0017】ついで、この結果得られた各種の被覆超硬
チップのうち、本発明被覆超硬チップ1〜16および従
来被覆超硬チップ1〜16について、
被削材:JIS・SUS304の丸棒、
切削速度:320m/min.、
切り込み:2.5mm、
送り:0.25mm/rev.、
切削時間:10分、
の条件でのステンレス鋼の乾式高速連続高切込み旋削加
工試験、
被削材:JIS・SUS304の長さ方向等間隔4本縦
溝入り丸棒、
切削速度:200m/min.、
切り込み:1.3mm、
送り:0.5mm/rev.、
切削時間:3分、
の条件でのステンレス鋼の乾式高速断続高送り旋削加工
試験、さらに、
被削材:JIS・S15Cの長さ方向等間隔4本縦溝入
り丸棒、
切削速度:280m/min.、
切り込み:1.5mm、
送り:0.55mm/rev.、
切削時間:5分、
の条件での軟鋼の乾式高速断続高送り旋削加工試験を行
い、いずれの旋削加工試験でも切刃の逃げ面摩耗幅を測
定した。────────────────────────────────────────────────── ───
[Procedure amendment] [Date of submission] August 22, 2001 (2001.8.2
2) [Procedure amendment 1] [Document name to be amended] Specification [Item name to be amended] 0017 [Correction method] Change [Content of amendment] Next, among the various coated carbide tips obtained as a result, Worked material: JIS SUS304 round bar, Cutting speed: 320 m / min. , Notch: 2.5 mm , feed: 0.25 mm / rev. , Cutting time: 10 minutes, Dry high-speed continuous high-depth turning test of stainless steel under the following conditions: Work material: JIS · SUS304 round bar with four longitudinal grooves at regular intervals in the longitudinal direction, Cutting speed: 200 m / min . Infeed: 1.3 mm Feed: 0.5 mm / rev. , Cutting time: 3 minutes, Dry high-speed intermittent high-feed turning test of stainless steel under the following conditions: Work material: JIS S15C, lengthwise round bar with four longitudinal grooves, Cutting speed: 280 m / Min. Infeed: 1.5 mm Feed: 0.55 mm / rev. A dry high-speed intermittent high-feed turning test of mild steel was performed under the following conditions: cutting time: 5 minutes, and the flank wear width of the cutting edge was measured in each turning test.
───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.7 識別記号 FI テーマコート゛(参考) C23C 14/32 C23C 14/32 F (72)発明者 田中 裕介 兵庫県明石市魚住町金ヶ崎西大池179番地 1 エムエムシーコベルコツ−ル株式会社 内 Fターム(参考) 3C037 CC02 CC04 CC11 3C046 FF03 FF05 FF10 FF17 FF19 FF25 4K029 AA04 BA41 BA54 BA58 BB02 BC02 BD05 CA03 DD06 EA01──────────────────────────────────────────────────続 き Continued on the front page (51) Int.Cl. 7 Identification symbol FI theme coat ゛ (Reference) C23C 14/32 C23C 14/32 F (72) Inventor Yusuke Tanaka 179 Kanegasaki Nishi-Oike, Uozumi-cho, Akashi-shi, Hyogo Prefecture 1 FMC Term Co., Ltd. F term (reference) 3C037 CC02 CC04 CC11 3C046 FF03 FF05 FF10 FF17 FF19 FF25 4K029 AA04 BA41 BA54 BA58 BB02 BC02 BD05 CA03 DD06 EA01
Claims (1)
化チタン基サーメットで構成された工具基体の表面に、 (a)組成式:(Ti1-XAlX)Nおよび同(Ti1-X
AlX)C1-YNY、で表わした場合、厚さ方向断面中央
部をオージェ分光分析装置で測定して、以下いずれも原
子比で、 X:0.1〜0.7、 Y:0.5〜0.99、 を満足するTiとAlの複合窒化物層およびTiとAl
の複合炭窒化物層のうちのいずれか、または両方からな
り、かつ0.5〜15μmの平均層厚を有する硬質被覆
層、 (b)組成式:(Ti1-aAla)C1-bObおよび同(T
i1-aAla)C1-(b+c)ObNcで表わした場合、厚さ方
向断面中央部をオージェ分光分析装置で測定して、 a:0.1〜0.7、 b:0.1〜0.8、 c:0.05〜0.65、 を満足するTiとAlの複合炭酸化物層および複合炭窒
酸化物層のうちの1種のまたは2種以上のからなり、か
つ0.1〜10μmの平均層厚を有する中間密着被覆
層、 (c)組成式:(Zr1-mMm)On(ただし、MはT
i、V、Nb、およびTaのうちの1種または2種以上
を示す)、で表わした場合、厚さ方向断面中央部をオー
ジェ分光分析装置で測定して、 m:0.01〜0.1、 n:1.7〜2.3、 を満足するZrとMの複合酸化物層からなり、かつ0.
5〜15μmの平均層厚を有する表面潤滑被覆層、以上
(a)〜(c)からなる被覆層を物理蒸着してなる、切
粉に対する表面潤滑性にすぐれた表面被覆超硬合金製切
削工具。Claims: 1. A surface of a tool base composed of a tungsten carbide-based cemented carbide or a titanium carbonitride-based cermet, wherein (a) a composition formula: (Ti 1-X Al X ) N (Ti 1-X
Al x ) C 1 -Y N Y , where the center of the cross section in the thickness direction was measured with an Auger spectrometer, and the following were all expressed in atomic ratios: X: 0.1 to 0.7; A composite nitride layer of Ti and Al satisfying 0.5 to 0.99, and Ti and Al
Any of a composite carbonitride layer, or consist of both, and a hard coating layer having an average layer thickness of 0.5 to 15 m, (b) the composition formula: (Ti 1-a Al a ) C 1- b Ob and the same (T
i 1-a Al a ) C 1- (b + c) O b N c , when measured at the center of the cross section in the thickness direction with an Auger spectrometer, a: 0.1 to 0.7; b: 0.1 to 0.8, c: 0.05 to 0.65, from one or more of the Ti and Al composite carbonate layers and composite carbonitride layers. It becomes, and the intermediate adhesion coating layer having an average layer thickness of 0.1 to 10 [mu] m, (c) the composition formula: (Zr 1-m M m ) O n ( however, M is T
i, V, Nb, and Ta, or one or more of Ta)), and the center of the cross section in the thickness direction is measured by an Auger spectroscopic analyzer. 1, n: a composite oxide layer of Zr and M satisfying 1.7 to 2.3;
Surface lubricating coating layer having an average layer thickness of 5 to 15 μm, and a surface-coated cemented carbide cutting tool having excellent surface lubricating properties against chips, obtained by physical vapor deposition of the coating layer comprising (a) to (c) above. .
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2001211733A JP3531627B2 (en) | 2001-07-12 | 2001-07-12 | Surface-coated cemented carbide cutting tool with excellent surface lubricity to chips |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2001211733A JP3531627B2 (en) | 2001-07-12 | 2001-07-12 | Surface-coated cemented carbide cutting tool with excellent surface lubricity to chips |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2003025110A true JP2003025110A (en) | 2003-01-29 |
| JP3531627B2 JP3531627B2 (en) | 2004-05-31 |
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ID=19046996
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2001211733A Expired - Fee Related JP3531627B2 (en) | 2001-07-12 | 2001-07-12 | Surface-coated cemented carbide cutting tool with excellent surface lubricity to chips |
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| Country | Link |
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| JP (1) | JP3531627B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8206812B2 (en) | 2006-12-15 | 2012-06-26 | Sandvik Intellectual Property Ab | Coated cutting tool |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3899500B2 (en) | 1999-04-09 | 2007-03-28 | 三菱マテリアル株式会社 | Cutting tool made of surface-coated carbide material that exhibits excellent wear resistance in high heat generation cutting |
| JP3899501B2 (en) | 1999-05-10 | 2007-03-28 | 三菱マテリアル株式会社 | Cutting tool made of surface-coated carbide material that exhibits excellent wear resistance in high heat generation cutting |
| JP2002254205A (en) | 2001-02-23 | 2002-09-10 | Mmc Kobelco Tool Kk | Surface-coated cemented carbide cutting tool having excellent surface lubricating property for chip |
-
2001
- 2001-07-12 JP JP2001211733A patent/JP3531627B2/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8206812B2 (en) | 2006-12-15 | 2012-06-26 | Sandvik Intellectual Property Ab | Coated cutting tool |
Also Published As
| Publication number | Publication date |
|---|---|
| JP3531627B2 (en) | 2004-05-31 |
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